Force sensor temperature compensation

ABSTRACT

In one embodiment, a force sensor apparatus is provided including a tube portion having a plurality of radial ribs and at least one fiber optic strain gauge positioned over each rib of the plurality of radial ribs. The strain gauges are comprised of a negative thermo-optic coefficient optical fiber material in one embodiment. A proximal end of the tube portion is operably couplable to a shaft of a surgical instrument that is operably couplable to a manipulator arm of a robotic surgical system, and a distal end of the tube portion is proximally couplable to a wrist joint coupled to an end effector. In another embodiment, adjacent fiber optic strain gauges with differing thermal responses are used to solve simultaneous equations in strain and temperature to derive strain while rejecting thermal effects. In yet another embodiment, a thermal shunt shell is over an outer surface of the tube portion. An advantageous surgical instrument having improved temperature compensation is also provided.

CROSS-REFERENCE TO RELATED APPLICATIONS AND PATENTS

This application is a continuation-in-part of U.S. application Ser. No. 11/958,772, filed Dec. 18, 2007, which is incorporated by reference herein for all purposes.

This application is related to U.S. Provisional Application No. 60/755,108 filed Dec. 30, 2005, U.S. Provisional Application 60/755,157 filed Dec. 30, 2005, U.S. application Ser. No. 11/553,303 filed Oct. 26, 2006, U.S. patent application Ser. No. 11/537,241 filed Sep. 29, 2006, U.S. patent application Ser. No. 11/093,372 filed Mar. 30, 2005, and U.S. Pat. Nos. 6,936,042, 6,902,560, 6,879,880, 6,866,671, 6,817,974, 6,783,524, 6,676,684, 6,371,952, 6,331,181, and 5,807,377, the full disclosures of which are incorporated by reference herein for all purposes.

TECHNICAL FIELD

The present invention relates generally to surgical robot systems and, more particularly, to an improved system, apparatus, and method for sensing forces applied to a surgical instrument.

BACKGROUND

In robotically-assisted surgery, the surgeon typically operates a master controller to control the motion of surgical instruments at the surgical site from a location that may be remote from the patient (e.g., across the operating room, in a different room or a completely different building from the patient). The master controller usually includes one or more hand input devices, such as handheld wrist gimbals, joysticks, exoskeletal gloves, handpieces, or the like, which are operatively coupled to the surgical instruments through a controller with servo motors for articulating the instruments' position and orientation at the surgical site. The servo motors are typically part of an electromechanical device or surgical manipulator arm (“the slave”) that includes a plurality of joints, linkages, etc., that are connected together to support and control the surgical instruments that have been introduced directly into an open surgical site or through trocar sleeves (cannulas) inserted through incisions into a body cavity, such as the patient's abdomen. There are available a variety of surgical instruments, such as tissue graspers, needle drivers, electrosurgical cautery probes, etc., to perform various functions for the surgeon, e.g., retracting tissue, holding or driving a needle, suturing, grasping a blood vessel, dissecting, cauterizing, coagulating tissue, etc. A surgeon may employ a large number of different surgical instruments/tools during a procedure.

This new surgical method through remote manipulation has created many new challenges. One such challenge is providing the surgeon with the ability to accurately “feel” the tissue that is being manipulated by the surgical instrument via the robotic manipulator. The surgeon must rely on visual indications of the forces applied by the instruments or sutures. It is desirable to sense the forces and torques applied to the tip of the instrument, such as an end effector (e.g., jaws, grasper, blades, etc.) of robotic minimally invasive surgical instruments, in order to feed the forces and torques back to the surgeon user through the system hand controls or by other means, such as visual display, vibrations, or audible tone. One device for this purpose from the laboratory of G. Hirzinger at DLR Institute of Robotics and Mechatronics is described in “Review of Fixtures for Low-Invasiveness Surgery” by F. Cepolina and R. C. Michelini, Int'l Journal of Medical Robotics and Computer Assisted Surgery, Vol. 1, Issue 1, page 58, the contents of which are incorporated by reference herein for all purposes. However, that design disadvantageously places a force sensor distal to (or outboard of) the wrist joints, thus requiring wires or optic fibers to be routed through the flexing wrist joint and also requiring the yaw and grip axes to be on separate pivot axes.

Another problem has been fitting and positioning the necessary wires, rods, or tubes for mechanical actuation of end effectors in as small a space as possible because relatively small instruments are typically desirable for performing surgery.

Furthermore, the temperature sensitivity of force sensors has caused problems with providing accurate force measurements.

What is needed, therefore, are improved telerobotic systems, surgical apparatus, and methods for remotely controlling surgical instruments at a surgical site on a patient. In particular, these systems and methods should be configured to provide accurate feedback of forces and torques to the surgeon to improve user awareness and control of the instruments.

SUMMARY

The present invention provides an apparatus, system, and method for improving force and torque feedback to and sensing by a surgeon performing a robotic surgery. In one embodiment, a force sensor includes a tube portion that includes a plurality of radial ribs and a strain gauge or gauges positioned over each of the plurality of radial ribs. A proximal part of the tube portion is coupled to a shaft of a surgical instrument that may be operably coupled to a manipulator arm of a robotic surgical system. A distal part of the tube portion is coupled to a wrist joint coupled to an end effector. The couplings may be direct or indirect with an intermediate mechanical component between the coupled parts.

Groups of strain gauges are positioned on or near a distal end of an instrument shaft proximal to (i.e., inboard of) a moveable wrist of a robotic surgical instrument via an apparatus that senses forces and torques at the distal tip of the instrument without errors due to changes in the configuration of the tip (such as with a moveable wrist) or steady state temperature variations.

The force sensor apparatus may be comprised of advantageous materials, such as high thermal diffusivity material and negative or differing thermo-optic coefficient optical fiber material, and/or include thermal shielding/heat spreading designs to provide accurate force signals even under asymmetric transient thermal loads that may occur in surgery.

Advantageously, the present invention improves the sensing and feedback of forces to the surgeon and substantially eliminates the problem of passing delicate wires, or optic fibers through the flexible wrist joint of the instrument. A force sensor apparatus may be manufactured, tested, and calibrated as a separate modular component and brought together with other components in the conventional instrument assembly process. The force sensor apparatus may also be manufactured as an integrated part of the instrument shaft. In addition, it is possible to choose a material for the sensor structural member different from the material of the instrument shaft whose design considerations may compromise the mechanical and/or thermal properties required for the sensor.

The scope of the invention is defined by the claims, which are incorporated into this section by reference. A more complete understanding of embodiments of the present invention will be afforded to those skilled in the art, as well as a realization of additional advantages thereof, by a consideration of the following detailed description of one or more embodiments. Reference will be made to the appended sheets of drawings that will first be described briefly.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1A is a perspective view of a robotic surgical system in accordance with an embodiment of the present invention.

FIG. 1B is a perspective view of a robotic surgical arm cart system of the robotic surgical system in FIG. 1A in accordance with an embodiment of the present invention.

FIG. 1C is a front perspective view of a master console of the robotic surgical system in FIG. 1A in accordance with an embodiment of the present invention.

FIG. 2 is a perspective view of a surgical instrument including a force sensor apparatus operably coupled proximal (or inboard) to a wrist joint in accordance with an embodiment of the present invention.

FIG. 3A is a perspective view of a force sensor apparatus.

FIG. 3B illustrates the force sensor of FIG. 3A operably coupled to a shaft and end portion of a surgical instrument.

FIG. 3C illustrates the force sensor of FIG. 3A with a protective cover over a portion of the force sensor.

FIG. 4A is a perspective view of an inner tube of another force sensor apparatus.

FIG. 4B is a partial cross-sectional view of an outer tube/cover over the inner tube of FIG. 4A of the force sensor apparatus.

FIG. 4C shows intervening material between the inner and outer tubes of FIG. 4B of the force sensor apparatus and wires or optic fibers operably coupled to the force sensor apparatus.

FIG. 4D shows a partial cross-sectional view of the force sensor apparatus operably coupled proximal to (or inboard of) a wrist joint of a surgical instrument.

FIG. 5A is a perspective view of a force sensor apparatus in accordance with yet another embodiment of the present invention.

FIG. 5B illustrates an enlarged perspective view of a section of the force sensor apparatus of FIG. 5A.

FIG. 5C illustrates a cross-sectional view of the force sensor apparatus of FIG. 5A along line 5C-5C, and FIG. 5C1 illustrates a magnified section labeled 5C1 in FIG. 5C.

FIG. 5D illustrates a cross-sectional view of the force sensor apparatus of FIG. 5A along line 5D-5D.

FIG. 5E illustrates a strain relief for strain gauge wires or optic fibers in accordance with an embodiment of the present invention.

FIGS. 6A and 6B illustrate perspective views of another force sensor apparatus and an enlarged view of a portion of the force sensor apparatus in accordance with another embodiment of the present invention.

FIG. 6C illustrates an end view of the force sensor apparatus of FIGS. 6A and 6B including radial ribs positioned in non-uniform angles, and FIG. 6C1 illustrates a magnified section labeled 6C1 in FIG. 6C, in accordance with another embodiment of the present invention.

FIGS. 7A and 7B illustrate a perspective view and an end view of another force sensor apparatus including radial ribs positioned in non-uniform supplementary angles and exposed by apertures on the tube surface, and FIG. 7B1 illustrates a magnified section labeled 7B1 in FIG. 7B, in accordance with another embodiment of the present invention.

FIG. 8 illustrates an end view of another force sensor apparatus including three radial ribs in accordance with another embodiment of the present invention.

FIGS. 9A and 9B illustrate perspective views of another force sensor apparatus and an enlarged section of the force sensor apparatus, respectively, in accordance with another embodiment of the present invention.

FIG. 9C illustrates an end view of the force sensor apparatus of FIGS. 9A and 9B including radial ribs positioned in non-uniform supplementary angles and a central through passage in accordance with another embodiment of the present invention.

FIG. 10 illustrates a perspective cutaway view of another force sensor apparatus, including apertures exposing radial ribs and a concentric shell surrounding the sensor tube with an annular gap in accordance with an embodiment of the present invention.

FIGS. 11A-11C illustrate different views of another force sensor apparatus, including a concentric shell surrounding the sensor tube with an annular heat conducting rib in accordance with an embodiment of the present invention.

Embodiments of the present invention and their advantages are best understood by referring to the detailed description that follows. It should be appreciated that like reference numerals are used to identify like elements illustrated in one or more of the figures. It should also be appreciated that the figures may not be necessarily drawn to scale.

DETAILED DESCRIPTION

The present invention provides a multi-component system, apparatus, and method for sensing forces applied to tissue while performing robotically-assisted surgical procedures on a patient, particularly including open surgical procedures, neurosurgical procedures, and minimally invasive procedures, such as laparoscopy, arthroscopy, thoracoscopy, and the like. The apparatus and method of the present invention are particularly useful as part of a telerobotic surgical system that allows the surgeon to manipulate the surgical instruments through a servomechanism from a location remote from the patient. To that end, the combined manipulator apparatus or slave and surgical instrument of the present invention will usually be driven by a master having the same degrees of freedom (e.g., 3 degrees of freedom for position and 3 degrees of freedom for orientation plus grip) to form a telepresence system with force reflection or other scalar force magnitude display. A description of a suitable slave-master system can be found in U.S. Pat. No. 6,574,355, the complete disclosure of which is incorporated herein by reference for all purposes.

Referring to the drawings in detail, wherein like numerals indicate like elements, a robotic surgical system 10 is illustrated according to an embodiment of the present invention. As shown in FIGS. 1A through 1C, robotic system 10 generally includes one or more surgical manipulator assemblies 51 mounted to or near an operating table O and a master control assembly located at a surgeon's console 90 for allowing the surgeon S to view the surgical site and to control the manipulator assemblies 51. The system 10 will also include one or more viewing scope assemblies and a plurality of surgical instrument assemblies 54 (FIG. 2) adapted for being removably coupled to the manipulator assemblies 51 (discussed in more detail below). Robotic system 10 includes at least two manipulator assemblies 51 and preferably at least three manipulator assemblies 51. The exact number of manipulator assemblies 51 will depend on the surgical procedure and the space constraints within the operating room among other factors. As discussed in detail below, one of the assemblies 51 will typically operate a viewing scope assembly (e.g., in endoscopic procedures) for viewing the surgical site, while the other manipulator assemblies 51 operate surgical instruments 54 for performing various procedures on the patient.

The control assembly may be located at a surgeon's console 90 which is usually located in the same room as operating table O so that the surgeon may speak to his/her assistant(s) and directly monitor the operating procedure. However, it should be understood that the surgeon S can be located in a different room or a completely different building from the patient. The master control assembly generally includes a support, a monitor for displaying an image of the surgical site to the surgeon S, and one or more master(s) for controlling manipulator assemblies 51. Master(s) may include a variety of input devices, such as hand-held wrist gimbals, joysticks, gloves, trigger-guns, hand-operated controllers, voice recognition devices, or the like. Preferably, master(s) will be provided with the same degrees of freedom as the combined manipulator 51 and surgical instrument assemblies 54. In conjunction with the endoscopic view, this provides the surgeon with telepresence, the perception that the surgeon is immediately adjacent to and immersed in the surgical site, and intuitiveness, the perception that the master(s) are integral with the instruments 54 so that the surgeon has a strong sense of directly and intuitively controlling instruments 54 as if they are part of or held in his/her hands. Position, force, and tactile feedback sensors (not shown) may also be employed on instrument assemblies 54 to transmit position, force, and tactile sensations from the surgical instrument back to the surgeon's hands, ears, or eyes as he/she operates the telerobotic system. One suitable system and method for providing telepresence to the operator is described in U.S. Pat. No. 6,574,355, which has previously been incorporated herein by reference.

The monitor 94 (FIG. 1C) will be suitably coupled to the viewing scope assembly such that an image of the surgical site is provided adjacent the surgeon's hands on the surgeon console. Preferably, monitor 94 will display an image that is oriented so that the surgeon feels that he or she is actually looking directly down onto the operating site. To that end, an image of the surgical instruments 54 appears to be located substantially where the operator's hands are located. In addition, the real-time image is a stereo image such that the operator can manipulate the end effector via the hand control as if viewing the workspace in substantially true presence. The image simulates the viewpoint or orientation of an operator who is physically manipulating the surgical instruments 54.

A servo control is provided for transferring the mechanical motion of masters to manipulator assemblies 51. The servo control may be separate from, or integral with, manipulator assemblies 51. The servo control will usually provide force and torque feedback from the surgical instruments 51 to the hand-operated masters. In addition, the servo control may include a safety monitoring controller (not shown) to safely halt system operation, or at least inhibit all robot motion, in response to recognized undesirable conditions (e.g., exertion of excessive force on the patient, mismatched encoder readings, etc.). The servo control preferably has a servo bandwidth with a 3 dB cut off frequency of at least 10 Hz so that the system can quickly and accurately respond to the rapid hand motions used by the surgeon and yet to filter out undesirable surgeon hand tremors. To operate effectively with this system, manipulator assemblies 51 have a relatively low inertia, and the drive motors have relatively low ratio gear or pulley couplings. Any suitable conventional or specialized servo control may be used in the practice of the present invention, with those incorporating force and torque feedback being particularly preferred for telepresence operation of the system.

Referring to FIG. 2, a perspective view is shown of a surgical instrument 54 including a force sensor apparatus 100 operably coupled to a distal end of a rigid shaft 110 and proximal to a wrist joint 121 in accordance with an embodiment of the present invention. An end portion 120, such as a surgical end effector, is coupled to force sensor apparatus 100 via the wrist joint 121. A housing 150 is operably coupled to a proximal end of the rigid shaft 110 and includes an interface 152 which mechanically and electrically couples instrument 54 to the manipulator 51.

Referring now to FIGS. 3A-3C in conjunction with FIGS. 1A-1C and 2, an improved apparatus, system, and method for sensing and feedback of forces and/or torques to the surgeon will be described. FIG. 3A shows a perspective view of force sensor apparatus 100 including in one embodiment a tube 102 including a number (e.g., 3, 4, 6, or 8) of strain gauges 104 (e.g., 104 a and 104 b) mounted to a surface of tube 102 and oriented axially (parallel to the lengthwise axis z of the tube). FIG. 3B shows the force sensor apparatus 100 of FIG. 3A operably coupled to a shaft 110 and end portion 120 of a surgical instrument. FIG. 3C shows a cross-section view of force sensor apparatus 100 including a cover or sleeve 113 over tube 102.

Force sensor apparatus 100 is a separately manufacturable module or part adapted for incorporation as part of the shaft 110 of surgical instrument 54 at a prescribed distance from the tip where there may be an articulated wrist with specialized jaws, cutting devices, or other end portion 120. In one example, tube 102 may be made of a sufficiently strong material and may be spool shaped, including end portions 102 b, 102 c with a depressed portion 102 a therebetween that is smaller in diameter than end portions 102 b, 102 c. Strain gauges 104 may be mounted on the surface of depressed portion 102 a. Proximal tube portion 102 c operably couples to the shaft 110 of surgical instrument 54 and distal tube portion 102 b operably couples to a wrist joint 121. In one example, the diameter of the completed force sensor apparatus matches the diameter of the instrument shaft, thus allowing the entire assembly of the instrument (including the coupled force sensor apparatus) to pass through a cannula or a seal without added friction or snagging.

Force sensor apparatus 100 includes a through passage 109 for end portion actuation cables or rods. End features 108 of end portion 102 b insure secure mounting and angular alignment to the main instrument shaft or the wrist/jaw/other end portion sub-assembly of the instrument. Wire leads or optic fibers 116 (e.g., shielded twisted pairs, coax, or fiber) from the strain gauges 104 may be inlaid into grooves 112 in the tube 102 and matching grooves in the shaft 110 of the surgical instrument 54. The wire leads or optic fibers 116 may then be embedded in an adhesive bonding or potting compound such as epoxy.

In one embodiment, as illustrated in FIG. 3C, cover 113 is positioned over and encapsulates the mounted strain gauges 104 and other circuit elements on the surface of the tube 102, thereby providing mechanical and/or electrical protection of the sensors. In one example, cover 113 is a mechanically protective woven sleeve potted on depressed portion 102 a and is comprised of a woven resin impregnated fiberglass or metal braid electrical shielding.

As disclosed in U.S. patent application Ser. No. 11/537,241, filed Sep. 29, 2006, the contents of which have been previously incorporated by reference, strain gauges 104 may be spaced in a ring at intervals around the circumference of the tube 102 (e.g., 3 gauges at 120 degrees, 4 gauges at 90 degrees, or 4 gauges at 70 degrees and 110 degrees or other pairs of supplementary angles). The signals from the sensors are combined arithmetically in various sums and differences to obtain measures of transverse forces F_(x) and F_(y) (FIG. 3A) exerted upon the instrument tip and to reject axial force F_(z) and the torques T_(x) and T_(y) about the two axes perpendicular to the shaft axis (i.e., axes x and y). The measurement of the forces is made independent of the orientation and effective lever arm length of an articulated wrist mechanism 121 at the distal end of the instrument when two axially separated sets or rings of gauges are utilized and their signals are subtracted. Forces exerted against end portion 120 are detected by the force sensing elements via an interrogator 334 (FIG. 5E), which may be operably coupled to the servo control or to a processor 340 (FIG. 5E) for notifying the surgeon of these forces (e.g., via master(s) or a display). It is understood that by adding a second ring of similarly oriented gauges (e.g., two sets of 3 gauges or two sets of 4 gauges) at a different lengthwise axial position on the tube, additional load-induced bending moment information may be obtained, and dependence of the transverse force data Fx, Fy on instrument wrist length, orientation, and resulting jaw distance may be eliminated.

In one example, various strain gauge types may be used, including but not limited to conventional foil type resistance gauges, semiconductor gauges, optic fiber type gauges using Bragg grating or Fabry-Perot technology, or others, such as strain sensing surface acoustic wave (SAW) devices. Optic fiber Bragg grating (FBG) gauges may be advantageous in that two sensing elements may be located along one fiber at a known separation, thereby only requiring the provision of four fibers along the instrument shaft for eight gauges.

Both fiber technologies require an interrogator unit 334 that decodes the optically encoded strain information into electrical signals compatible with the computer control hardware 340 or display means of the robotic surgical system. A processor may then be used to calculate forces according to the signals from the strain gauges/sensors.

Additionally, there may be co-mounted unstrained gauges or Poisson strained gauges oriented in the circumferential direction adjacent to each axial gauge and incorporated in the bridge completion circuits to eliminate temperature effects. The strain gauge bridge circuits are completed in a manner to give the best signal for bending loads due to the lateral forces (F_(x) and F_(y)) exerted on the instrument tip jaws.

For resistive foil or semiconductor strain gauges, active components such as bare die op-amps and passive components such as secondary resistors or capacitors may be attached adjacent to the strain gauges connected by bond wires or thick film circuit traces in the manner of hybrid circuits to amplify, filter, and/or modulate the gauge output signals to reject noise sources. Such components are not needed for fiber optic gauges.

Housing 150 operably interfaces with a robotic manipulator arm 51, in one embodiment via a sterile adaptor interface 152 (FIG. 2). Applicable housings, sterile adaptor interfaces, and manipulator arms are disclosed in U.S. patent application Ser. No. 11/314,040 filed on Dec. 20, 2005, and U.S. application Ser. No. 11/613,800 filed on Dec. 20, 2006, the full disclosures of which are incorporated by reference herein for all purposes. Examples of applicable shafts, end portions, housings, sterile adaptors, and manipulator arms are manufactured by Intuitive Surgical, Inc. of Sunnyvale, Calif.

In a preferred configuration, end portion 120 has a range of motion that includes pitch and yaw motion about the x- and y-axes and rotation about the z-axis (axes shown in FIG. 3A). These motions as well as actuation of an end effector are provided via cables in housing 150 and cables and/or rods running through shaft 110 and into housing 150 that transfer motion from the manipulator arm 51. Embodiments of drive assemblies, arms, forearm assemblies, adaptors, and other applicable parts are described for example in U.S. Pat. Nos. 6,331,181, 6,491,701, and 6,770,081, the full disclosures of which are incorporated herein by reference for all purposes.

It is noted that various surgical instruments may be improved in accordance with the present invention, including but not limited to tools with and without end effectors, such as jaws, scissors, graspers, needle holders, micro-dissectors, staple appliers, tackers, suction irrigation tools, clip appliers, cutting blades, irrigators, catheters, and suction orifices. Alternatively, the surgical instrument may comprise an electrosurgical probe for ablating, resecting, cutting or coagulating tissue. Such surgical instruments are available from Intuitive Surgical, Inc. of Sunnyvale, Calif.

For the methods and apparatus mentioned above, it may be advantageous to use a calibration process in which combinations of forces and torques are applied to the instrument tip serially or in simultaneous combinations while correction factors and offsets are determined. The correction factors and offsets may then be applied to the theoretical equations for combining the gauge outputs to obtain F_(x), F_(y), and reject F_(z), T_(x), and T_(y). Such a calibration process may be done either by directly calculating the correction factors and offsets or by a learning system such as a neural network embedded in the calibration fixture or in the instrument itself. In any calibration method, the calibration data may be programmed into an integrated circuit embedded in the instrument so that the surgical system using the individual instrument can correctly identify and apply its correction factors and offsets while the instrument is in use.

Advantageously, force sensor apparatus 100 is adaptable to the size and shape constraints of various robotic surgical instruments and is suitable for a variety of instruments. Accordingly, end portions 102 b, 102 c may be formed into various applicable shapes and sizes. Furthermore, force sensor apparatus 100 may be manufactured, tested, and calibrated as a separate modular component and brought together with other components in the conventional instrument assembly process. Also, the sensor may be a slip-on module with suitable electrical contacts that mate with contacts on the instrument shaft permitting a higher value sensor to be used with lower cost instruments of limited cycle life. In addition, the sensor structural member 102 may be comprised of an advantageous material, which may be the same or a different material than the instrument shaft 110 whose design considerations may compromise the properties required for the sensor.

Referring now to FIGS. 4A through 4D, a force sensor apparatus 200 is illustrated. The descriptions of substantially similar parts or elements as those described above with respect to FIGS. 3A-3C are applicable in this embodiment with respect to FIGS. 4A-4D, and redundant descriptions may be omitted.

FIG. 4A is a perspective view of an inner tube 218 of force sensor apparatus 200. Inner tube 218 includes a proximal raised end portion 218 b and a depressed portion 218 a smaller in diameter than raised end portion 218 b. Strain gauges, as described above with respect to FIGS. 3A-3C, may be mounted on the surface of depressed portion 218 a. Raised end portion 218 b may include grooves 212 for routing of wire leads or optic fibers from strain gauges 204.

FIG. 4B is a partial cross-sectional view of an outer tube 214 over the inner tube 218. In one example, outer tube 214 can provide mechanical and thermal protection of strain gauges 204 on inner tube 218. FIG. 4C highlights elastomeric material 215 between inner tube 218 and outer tube 214 maintaining concentricity of the tubes. Leads or optic fibers 216 connecting gauges 204 with data acquisition means are inlaid into grooves 212 and may be potted in place with epoxy or other adhesive. Finally in FIG. 4D wrist 221 and end effector 220 are connected distally to tube 214.

Referring now to FIGS. 5A-5E, views of a surgical instrument including another force sensor apparatus 300 is illustrated in accordance with yet another embodiment of the present invention. An end portion 320, such as a surgical end effector, is coupled to force sensor apparatus 300 via a wrist joint 321. A housing 150 (FIG. 5E) is operably coupled to a proximal end of a rigid shaft 310, the housing 150 further including an interface 152 which mechanically and electrically couples the instrument to the manipulator 51 (FIG. 1B). FIG. 5B is an enlarged perspective view of an aperture and rib section of the force sensor apparatus of FIG. 5A. FIGS. 5C and 5D are cross-sectional views of the force sensor apparatus of FIG. 5A along lines 5C-5C and 5D-5D, respectively, and FIG. 5C illustrates a magnified section labeled 5C1 in FIG. 5C. FIG. 5E illustrates an example proximal portion of the surgical instrument including the housing and operably coupling of the instrument to an interrogator 334 and processor 340. The descriptions of substantially similar parts or elements as those described above with respect to FIGS. 1-4 are applicable in this embodiment with respect to FIGS. 5A-5E, although redundant descriptions may be omitted.

Returning to FIG. 5A, force sensor apparatus 300 includes a generally annular tube 306 operably coupled to a distal end of rigid shaft 310 and proximal to wrist joint 321 in accordance with an embodiment of the present invention. In one embodiment, tube 306 includes a number of rectangular-shaped apertures 301 cut from tube 306 and a plurality of radial ribs 302 forming through passages 308 for passage of actuation cables, wires, tubes, rods, cautery wires and/or flushing fluids. Ribs 302 run along and radiate from the z-axis centerline of tube 306, and a number (e.g., 3, 4, 6, or 8) of strain gauges 304 are oriented parallel to the lengthwise z-axis of the tube and mounted to an outer rib surface 302 a. The strain gauges may be inlaid into grooves or a depressed area 317 on the outer rib surface 302 a in one example.

In the embodiment illustrated in FIGS. 5A-5D, force sensor apparatus 300 includes two sets of four apertures 301 cut from the wall of tube 306 at separate axial locations along tube 306. Each of the ribs 302 are separated by 90 degrees measured about the z-axis centerline of tube 306, which forms a cruciform cross-sectional view of the ribs 302, as shown in FIGS. 5C and 5D. Ribs 302 form four through passages 308. Furthermore, ribs 302 may extend along the entire length of tube 306 thereby forming internal through passages 308 along the entire length of tube 306, or ribs 302 may extend along a portion(s) of the length of tube 306, thereby forming internal through passages along a portion or portions of the length of tube 306.

Force sensor apparatus 300 is capable of sensing bending moments due to lateral forces applied to the wrist joint 321 or its specialized end portion 320. Advantageously, apertures 301 and ribs 302 provide for regions of controlled stress and strain when subjected to bending moments, which may be measured by fiber optic strain gauges 304 embedded in grooves 317 along an outer surface of the ribs and sensor body parallel to the lengthwise z-axis of tube 306. Through passages 308 permit cables, wires, tubes, or rigid tendons to pass through the sensor apparatus body to actuate the distal wrist joint(s) and/or control the end portion.

In one example, tube 306 and ribs 302 may be made of a sufficiently strong but elastic material to allow sensing of stress and strain without mechanical failure. Tube 306 and ribs 302 are further comprised of material with a sufficiently low modulus of elasticity to give a sufficient strain signal under an applied load, a sufficiently high strain at yield to give adequate safety margin above the maximum design load, and a sufficiently high thermal diffusivity to promote rapid thermal equilibrium (therefore reducing thermal disturbances to sensor output signals) when subject to localized or asymmetric thermal disturbances from tissue contact or endoscope illumination. In particular, the plurality of radial ribs 302 may be comprised of a high thermal diffusivity material, such as an aluminum alloy (e.g., 6061-T6 aluminum) or a copper alloy (e.g., GlidCop® AL-60) or a silver alloy to reduce the temperature difference between opposing gauges under transient thermal disturbances by providing a direct thermal pathway between opposing gauges.

In one example, tube 306 may be comprised of metal alloys, treated metals, or plated metals, such as of aluminum, copper, or silver, which allow for adequate strain, mechanical failure safety margin, and high thermal diffusivity. In a further example, 6061-T6 aluminum, which is an aluminum alloy that is heat treated and aged, GlidCop® AL-60, which is copper that is dispersion strengthened with ultrafine particles of aluminum oxide, or a dispersion strengthened silver, may be used to form tube 306 and ribs 302. Accordingly, both the plurality of ribs and the tube 302 may be comprised of a high thermal diffusivity material, such as an aluminum alloy (e.g., 6061-T6 aluminum) or a copper alloy (e.g., GlidCop® AL-60) or silver alloy to reduce transient and/or steady-state temperature differences between groups of strain gauges separated along the z-axis.

Advantageously, the present invention allows for a low bending moment of inertia to increase a strain signal to noise signal ratio consistent with a materials choice and rib design meeting the need for high thermal diffusivity and a direct thermal path between opposing strain gauges while also providing passage for actuation cables, wires, tubes, and/or rods.

Wire leads or optic fibers 316 (e.g., shielded twisted pairs, coax, or fiber) coupled to the strain gauges 304 may be inlaid into grooves 317 on tube 306, the outer rib surface 302 a, and matching grooves 319 in shaft 310 of the surgical instrument. The wire leads or optic fibers 316 may then be embedded in an adhesive potting compound such as epoxy.

As disclosed in U.S. patent application Ser. No. 11/537,241, filed Sep. 29, 2006, the contents of which have been previously incorporated by reference, strain gauges 304 may be spaced in a ring at intervals around the circumference of the tube 306 mounted on ribs 302 (e.g., 3 gauges at 120 degrees, 4 gauges at 90 degrees, 4 gauges at 70 and 110 degrees or other supplementary pairs of angles). The signals from the sensors are combined arithmetically in various sums and differences to obtain measures of the transverse forces F_(x), F_(y), and to reject axial forces F_(z) exerted upon the instrument tip and to reject wrist torques about the two axes perpendicular to the shaft axis (i.e., axes x and y). In accordance with the present invention, the measurement of the transverse forces is made independent of the orientation and effective lever arm length of an articulated wrist mechanism at the distal end of the instrument as well as wrist friction moments and actuator cable tensions when two axially separated sets or rings of gauges are utilized. Forces exerted against end portion 320 are detected by the force sensing elements, which may be operably coupled to the servo control or surgeon display means via an interrogator 334 and to a processor 340 for notifying the surgeon of these forces (e.g., via master(s) or a display means). It is understood that by adding a second ring of similarly oriented gauges (e.g., two sets of 3 gauges or two sets of 4 gauges) at a different position along the z-axis of the tube, additional side load-induced moment information can be obtained, and dependence of the force data on instrument wrist length, orientation, and resulting jaw distance and cable tensions, can be eliminated.

In one example, various strain gauges may be used, including but not limited to conventional foil type resistance gauges, semiconductor gauges, optic fiber type gauges using Bragg grating or Fabry-Perot technology, or others, such as strain sensing surface acoustic wave (SAW) devices. Optic fiber Bragg grating (FBG) gauges may be advantageous in that two sensing elements may be located along one fiber at a known separation, thereby only requiring the provision of four fibers along the instrument shaft. Fiber optic gauges may also be desirable because of their immunity to disturbance from cautery and other electromagnetic noise.

A problem with the use of FBG strain gauges in conventional fiber such as SMF-28 is their inherent positive temperature sensitivity, being especially problematic when the FBG strain gauges are mounted to materials with a positive thermal expansion coefficient, which adds to the temperature sensitivity of the FGB strain gauges. Temperature sensitivity limits the accuracy of a force transducer utilizing FBGs and positive thermal expansion coefficient substrate materials, especially under asymmetric transient thermal loads that may occur in surgery.

Intrinsic and extrinsic temperature compensation of FBG strain sensors may be accomplished with additional gratings written in the same or nearby region of the fiber and may include the use of additional fibers, exotic doped fibers spliced together, highly bi-refringent fiber or other means to differentiate thermal responses so that simultaneous equations in strain and temperature with respect to wavelength shift can be solved to obtain the strain independent of the temperature of any single grating. These methods typically require additional interrogator channels or exotic interrogation methods.

In another example, the plurality of fiber optic strain gauges 304 may be comprised of a negative thermo-optic coefficient optical fiber material, such as binary or ternary phosphate glass fiber, fluoride glass fiber, oxy-fluoride glass fiber, tellurite glass fiber, or a polymer fiber. The negative thermo-optic coefficient fiber advantageously reduces or eliminates the combined effect of a positive thermo-optic coefficient fiber, such as SMF-28 or other doped fiber, and the positive thermal expansion coefficient of the sensor body material.

Advantageously, embodiments of the present invention provide apparatus and methods for improved thermal stability when subjected to temperature changes, such as when entering the patient body from a lower temperature operating room environment, contacting warm living tissue, absorbing incident light from an endoscope illuminator, or other source of thermal disturbance that may occur during surgery. Also, the present invention provides for cost savings, relative ease of manufacture, higher field reliability, and accurate strain measurements.

Both FBG and Fabry-Perot fiber technologies require an interrogator unit, such as interrogator unit 334 (FIG. 5E) that decodes the optically encoded strain information into electrical signals compatible with the computer control hardware of the robotic surgical system. A processor 340 (FIG. 5E) operably coupled to the interrogator unit 334 may then be used to calculate forces according to the signals from the strain gauges/sensors.

For resistive foil or semiconductor strain gauges, active components such as bare die op-amps and passive components such as secondary resistors or capacitors may be attached adjacent to the strain gauges connected by bond wires or thick film circuit traces in the manner of hybrid circuits to amplify, filter, and/or modulate the gauge output signals to reject noise sources. Such components are not needed for fiber optic gauges.

In accordance with an embodiment of the present invention, force sensor apparatus 300 is a separately manufactured module or part adapted for incorporation as part of the shaft 310 of a laparoscopic surgical instrument at a prescribed distance from the tip where there may be an articulated wrist with specialized jaws, cutting devices, or other end portion 320. A proximal portion of tube 306 operably couples to the shaft 310 of the surgical instrument and a distal portion of tube 306 operably couples to wrist joint 321. In one example, the diameter of the completed force sensor apparatus matches the diameter of the instrument shaft, thus allowing the entire assembly of the instrument (including the coupled force sensor apparatus) to pass through a cannula or a seal without added friction or snagging. In other embodiments, the surgical instrument may be manufactured with a force sensor portion integrated as a part of shaft 310 (i.e., force sensor apparatus 300 is not separable from the shaft).

Similar to the embodiments described above, the surgical instrument to which force sensor apparatus 300 couples may also include a service loop 330 (FIG. 5E) of conductive traces or optic fibers at the proximal end of the instrument shaft 310 and a cable swivel mechanism 332 permitting the substantially free rotation of the instrument shaft while conducting the input gauge excitation power or light and electrical or optical output gauge signals to the interrogator unit 334.

Similar to the embodiments described above, the housing 150 operably interfaces with a robotic manipulator arm, in one embodiment via a sterile adaptor interface. Applicable housings, sterile adaptor interfaces, and manipulator arms are disclosed in U.S. patent application Ser. No. 11/314,040 filed on Dec. 20, 2005, and U.S. patent application Ser. No. 11/613,800 filed on Dec. 20, 2006, the full disclosures of which are incorporated by reference herein for all purposes. Examples of applicable shafts, end portions, housings, sterile adaptors, and manipulator arms are manufactured by Intuitive Surgical, Inc. of Sunnyvale, Calif.

In a preferred configuration, end portion 320 has a range of motion that includes pitch and yaw motion about the x- and y-axes and rotation about the z-axis. These motions as well as actuation of an end effector are provided via cables in the housing 150 and cables and/or rods running through the shaft and into the housing that transfer motion from the manipulator arm. Embodiments of drive assemblies, arms, forearm assemblies, adaptors, and other applicable parts are described for example in U.S. Pat. Nos. 6,331,181, 6,491,701, and 6,770,081, the full disclosures of which are incorporated herein by reference for all purposes.

It is noted that various surgical instruments may be improved in accordance with the present invention, including but not limited to tools with and without end effectors, such as jaws, scissors, graspers, needle holders, micro-dissectors, staple appliers, tackers, suction irrigation tools, clip appliers, cutting blades, hooks, sealers, lasers, irrigators, catheters, and suction orifices. Alternatively, the surgical instrument may comprise an electrosurgical probe for ablating, resecting, cutting or coagulating tissue. Such surgical instruments are manufactured by Intuitive Surgical, Inc. of Sunnyvale, Calif.

For the sensing methods and apparatus mentioned above, it may be advantageous to use a calibration process in which combinations of forces and torques are applied to the instrument tip serially, simultaneously, or in combinations while correction factors and offsets are determined to apply to the theoretical equations for combining the gauge outputs to obtain F_(x), F_(y) and reject F_(z), T_(x), and T_(y). This calibration may be done either by directly calculating the correction factors and offsets or by a learning system such as a neural network embedded in the calibration fixture or in the instrument itself. In any calibration method, the calibration data may be programmed into an integrated circuit embedded in the instrument so that the surgical system using the individual instrument can correctly identify and apply its correction factors and offsets while the instrument is in use.

Advantageously, force sensor apparatus 300 of the present invention is adaptable to the size and shape constraints of robotic endoscopic surgical instruments and is suitable for a variety of instruments. Furthermore, force sensor apparatus 300 may be manufactured, tested, and calibrated as a separate modular component and brought together with other components in the conventional instrument assembly process or as an integrated part of the instrument shaft 310. Also, the sensor may be a slip-on module permitting a higher value sensor to be used with lower cost instruments of limited cycle life.

The present invention is not limited to rib orientation or a certain number of ribs, sets of ribs, strain gauges, or tube apertures, and FIGS. 6A-6C1, 7A-7B1, 8, and 9A-9C illustrate force sensor apparatus in accordance with other embodiments of the present invention. The descriptions of substantially similar parts or elements as those described above with respect to FIGS. 5A-5E are applicable in these embodiments although redundant descriptions may be omitted.

Referring now to FIGS. 6A-6C1, a force sensor apparatus 400 is illustrated, the force sensor apparatus 400 including four ribs 402 in diametrically opposite pairs at skewed supplementary angles (e.g., 70 degrees and 110 degrees) about a z-axis centerline of a tube 406. Ribs 402 extend radially within tube 406 from the z-axis centerline of the tube providing four through passages 408 a and 408 b for passage of actuation cables, wires, tubes, rods, cautery wires and/or flushing fluids. Advantageously, a larger through passage 408 a utilizing skewed angles allows for easier passage of cables, wires, tubes, and/or rods through tube 406 (e.g., three hypodermic tubes may be passed per 110 degree channel). In this embodiment, as can be seen in FIG. 6A, tube 406 does not include apertures through the wall of tube 406. However, the combined stiffness of tube 406 and ribs 402 still allow for a strong strain signal to noise signal ratio consistent with a materials choice and rib design meeting the need for high thermal diffusivity and a direct thermal path between opposing strain gauges while also providing passage for actuation cables, wires, tubes, and/or rods.

Similar to the embodiments disclosed above, a number of strain gauges 404 are oriented parallel to the lengthwise z-axis of the tube and mounted to an outer rib surface 402 a. The strain gauges may be inlaid into grooves or a depressed area 417 on the outer rib surface 402 a in one example. Wire leads or optic fibers 416 (e.g., shielded twisted pairs, coax, or fiber) coupled to the strain gauges 404 may be inlaid into grooves 417 on the outer rib surface 402 a of tube 406. The wire leads or optic fibers 416 may then be embedded in an adhesive potting compound such as epoxy.

Referring now in particular to FIGS. 6C and 6C1, an end view of force sensor apparatus 400 and a magnified section labeled 6C1 in FIG. 6C are respectively illustrated. A thermal shielding over the strain gauges may be provided in accordance with another embodiment of the present invention. In one example, a thermal shunt shell 452 is provided over tube 406 with an insulating fluid (gas or liquid) filled or evacuated gap 450 being provided between the outer surface of tube 406 and the inner surface of thermal shunt shell 452. Thermal shunt shell 452 may be comprised of a high thermal diffusivity material, such as an aluminum alloy (e.g., 6061-T6 aluminum) or a copper alloy (e.g., GlidCop® AL-60) or a silver alloy. Optionally, a light reflective surface or coating 453 may be provided over thermal shunt shell 452, which may deflect light and reduce localized heating of the force sensor apparatus, for example from endoscope illumination. An insulating coating 454 may also be provided over thermal shunt shell 452, the insulating coating 454 being comprised of a substantially transparent plastic shrink polymer in one example. Advantageously, the thermal shielding over the sensor tube 406 and the strain gauges 404 as described above allows for more uniform heat/thermal diffusion among the gauges, being particularly advantageous for mitigating asymmetric thermal loads upon the instrument. The thermal shielding described above is applicable for various embodiments of the present invention.

Referring now to FIGS. 7A thru 7B1, a force sensor apparatus 500 is illustrated, the force sensor apparatus 500 including four ribs 502 paired at skewed angles (e.g., 70 degrees and 110 degrees) about a z-axis centerline of a tube 506. Ribs 502 extend radially within tube 506 from the z-axis centerline of the tube providing four through passages 508 a and 508 b for passage of actuation cables, wires, tubes, rods cautery wires and/or flushing fluids. Advantageously, a larger through passage 508 a utilizing skewed angles allows for easier passage of cables, wires, tubes, and/or rods through tube 506 (e.g., three hypodermic tubes may be passed per 110 degree channel). In this embodiment, as can be seen in FIG. 7A, tube 506 include apertures 501 provided through the wall of tube 506. The reduced stiffness of exposed ribs 502 allow for a strong strain signal to noise signal ratio consistent with a materials choice and rib design meeting the need for high thermal diffusivity and a direct thermal path between opposing strain gauges while also providing passage for actuation cables, wires, tubes, rods, and the like.

Similar to the embodiments disclosed above, a number of strain gauges 504 are oriented parallel to the lengthwise z-axis of the tube and mounted to an outer rib surface 502 a. The strain gauges may be inlaid into grooves or a depressed area 517 on the outer rib surface 502 a in one example. Wire leads or optic fibers 516 (e.g., shielded twisted pairs, coax, or fiber) coupled to the strain gauges 504 may be inlaid into grooves 517 on tube 506, the outer rib surface 502 a, and matching grooves 517 in a shaft of the surgical instrument. The wire leads or optic fibers 516 in grooves 517 may then be embedded in an adhesive potting compound such as epoxy.

FIG. 8 illustrates a cross-sectional view of another force sensor apparatus which includes three ribs 602 separated by 120 degrees about a z-axis centerline of the force sensor apparatus tube 606. Ribs 602 provide three through passages 608. Wire leads or optic fibers 616 (e.g., shielded twisted pairs, coax, or fiber) coupled to strain gauges may be inlaid into grooves 617 on an instrument tube, an outer rib surface, and matching grooves in a shaft of the surgical instrument.

Referring now to FIGS. 9A-9C, a force sensor apparatus 700 is illustrated, the force sensor apparatus 700 including four ribs 702 paired at skewed angles (e.g., 70 degrees and 110 degrees) about a z-axis centerline of a tube 706. Ribs 702 extend radially within tube 706 from the z-axis centerline of the tube providing through passages 708 a and 708 b. In this embodiment, force sensor apparatus 700 also includes a central through passage 708 c along a lengthwise axis of tube 706 in accordance with another embodiment of the present invention. The through passages may be used for passage of actuation cables, wires, tubes, rods, and/or fluids. In this embodiment, as can be seen in FIG. 9A, tube 706 does not include apertures through the wall of the tube but apertures exposing portions of the interior ribs are within the scope of the present invention. Furthermore, the combined stiffness of tube 706 and ribs 702 still allow for a strong strain signal to noise signal ratio consistent with a materials choice and rib design meeting the need for high thermal diffusivity and a thermal path between opposing strain gauges while also providing passage for actuation cables, wires, tubes, rods, and/or fluids.

Similar to the embodiments disclosed above, a number of strain gauges 704 are oriented parallel to the lengthwise z-axis of the tube and mounted to an outer rib surface 702 a. The strain gauges may be inlaid into grooves or a depressed area 717 on the outer rib surface 702 a in one example. Wire leads or optic fibers 716 (e.g., shielded twisted pairs, coax, or fiber) coupled to the strain gauges 704 may be inlaid into grooves 717 on the outer rib surface 702 a of tube 706. The wire leads or optic fibers 716 may then be embedded in an adhesive potting compound such as epoxy.

Referring now to FIG. 10, a perspective cutaway view of another force sensor apparatus is illustrated in accordance with an embodiment of the present invention. The descriptions of substantially similar parts or elements as those described above with respect to FIGS. 1A-9C are applicable in this embodiment with respect to FIG. 10, although redundant descriptions may be omitted. Force sensor apparatus 800 includes a generally annular tube 806 operably coupled to an end portion 820 via a wrist joint 821. In this embodiment, tube 806 includes a number of rectangular-shaped apertures 801 cut from tube 806 and a plurality of radial ribs 802 forming through passages 808 for passage of wrist actuation cables, wires, tubes, or rods, cautery wires and/or flushing fluids. Ribs 802 run along and radiate from the z-axis centerline of tube 806, and a plurality of strain gauges 804 are oriented parallel to the lengthwise z-axis of the tube and mounted to an outer rib surface 802 a. The strain gauges may be inlaid into grooves or a depressed area 817 on the outer rib surface 802 a in one example. Wire leads or optic fibers 816 (e.g., shielded twisted pairs, coax, or fiber) coupled to the strain gauges 804 may be inlaid into grooves 817 on the outer rib surface 802 a of tube 806. The wire leads or optic fibers 816 may then be embedded in an adhesive potting compound such as epoxy.

In this embodiment, each of the ribs 802 are separated by 90 degrees measured about the z-axis centerline of tube 806, which forms a cruciform cross-sectional view of the ribs 802. Other separation angles for the ribs are within the scope of the present invention, as outlined above. Furthermore, ribs 802 may extend along the entire length of tube 806 thereby forming internal through passages 808 along the entire length of tube 806, or ribs 802 may extend along a portion(s) of the length of tube 806, thereby forming internal through passages along a portion or portions of the length of tube 806.

Similar to the embodiments described above, force sensor apparatus 800 is capable of sensing bending moments due to lateral forces applied to the wrist joint 821 or its specialized end portion 820. Advantageously, apertures 801 and ribs 802 provide for regions of controlled stress and strain when subjected to bending moments, which may be measured by the fiber optic strain gauges 804 embedded in the grooves 817 along the outer surface of the ribs and sensor body parallel to the lengthwise z-axis of tube 806.

In one example, tube 806 and ribs 802 may be comprised of material with a sufficiently low modulus of elasticity to give a sufficient strain signal under an applied load, a sufficiently high strain at yield to give adequate safety margin above the maximum design load, and a sufficiently high thermal diffusivity to promote rapid thermal equilibrium (therefore reducing thermal disturbances to sensor output signals) when subject to localized or asymmetric thermal disturbances from tissue contact or endoscope illumination. In particular, the plurality of radial ribs 802 may be comprised of a high thermal diffusivity material, such as an aluminum alloy (e.g., 6061-T6 aluminum) or a copper alloy (e.g., GlidCop® AL-60) or silver alloy to reduce the temperature difference between opposing gauges under transient thermal disturbances by providing a direct thermal pathway between opposing gauges. In yet another example, the plurality of fiber optic gauges 804 may be comprised of a negative thermo-optic coefficient optical fiber material, such as binary or ternary phosphate glass fiber, fluoride glass fiber, oxy-fluoride glass fiber, tellurite glass fiber, or a polymer fiber. The negative thermo-optic coefficient fiber advantageously reduces or eliminates the combined effect of a positive thermo-optic coefficient fiber, such as SMF-28 or other doped fiber, and the positive thermal expansion coefficient of the sensor body material.

In one example, tube 806 may be comprised of metal alloys, treated metals, or plated metals, such as of aluminum, copper, or silver, which allow for adequate strain, mechanical failure safety margin, and high thermal diffusivity. In a further example, 6061-T6 aluminum, which is an aluminum alloy that is heat treated and aged, GlidCop® AL-60, which is copper that is dispersion strengthened with ultrafine particles of aluminum oxide, or a dispersion strengthened silver, may be used to form both tube 806 and ribs 802. Accordingly, both the plurality of ribs 802 and the tube 806 may be comprised of a high thermal diffusivity material, such as an aluminum alloy (e.g., 6061-T6 aluminum) or a copper alloy (e.g., GlidCop® AL-60) or silver alloy, to reduce transient and/or steady-state temperature differences between groups of strain gauges separated along the z-axis.

Similar to the embodiment described above with respect to FIGS. 6A-6C1, a thermal shielding may be provided over the strain gauges 804 in accordance with another embodiment of the present invention. In one example, a thermal shunt shell 852 is provided over tube 806 with an insulating fluid (gas or liquid) filled or evacuated gap 850 being provided between the outer surface of tube 806 and the inner surface of thermal shunt shell 852. Thermal shunt shell 852 may be mechanically and thermally isolated from the strain gauges by providing compliant elastomer rings 830 between the shunt shell 852 and the tube 806 to prevent interference with the applied surgical forces and to insulate the sensor. Thermal shunt shell 852 may be comprised of a high diffusivity material, such as an aluminum alloy (e.g., 6061-T6 aluminum) or a copper alloy (e.g., GlidCop® AL-60) or silver alloy. Optionally, a light reflective surface or coating may be provided over thermal shunt shell 852, which may deflect light and reduce localized heating of the force sensor apparatus, for example from endoscope illumination. An insulating coating may also be provided over thermal shunt shell 852, the insulating coating being comprised of a substantially transparent plastic shrink polymer in one example. Advantageously, the thermal shielding over the strain gauges as described above allows for more uniform heat/thermal diffusion among the sensors, being particularly advantageous for mitigating asymmetric or transient thermal loads upon the instrument. The thermal shielding described above is applicable for various embodiments of the present invention.

Referring now to FIGS. 11A-11C, different views of another force sensor apparatus is illustrated in accordance with an embodiment of the present invention. The descriptions of substantially similar parts or elements as those described above with respect to FIGS. 1A-10 are applicable in this embodiment with respect to FIGS. 11A-11C, although redundant descriptions may be omitted. A force sensor apparatus 900 includes a generally annular tube 906 operably coupled to an end effector via a wrist joint 921. In this embodiment, tube 906 includes a plurality of radial ribs forming through passages for passage of wrist actuation cables, wires, tubes, or rods, cautery wires, flushing fluids, and the like. A plurality of strain gauges 904 are oriented parallel to the lengthwise z-axis of the tube and mounted to an outer rib surface. The strain gauges may be inlaid into grooves or a depressed area 917 on the outer rib surface in one example. Wire leads or optic fibers 916 (e.g., shielded twisted pairs, coax, or fiber) coupled to the strain gauges 904 may be inlaid into grooves 917 on the outer rib surface of tube 906. The wire leads or optic fibers 916 may then be embedded in an adhesive potting compound such as epoxy.

In this embodiment, each of the ribs may be separated by 90 degrees measured about the z-axis centerline of tube 906, which forms a cruciform cross-sectional view of the ribs. Other separation angles for the ribs are within the scope of the present invention, as outlined above. Furthermore, the ribs may extend along the entire length of tube 906 thereby forming internal through passages along the entire length of tube 906, or the ribs may extend along a portion(s) of the length of tube 906, thereby forming internal through passages along a portion or portions of the length of tube 906.

Similar to the embodiments described above, force sensor apparatus 900 is capable of sensing bending moments due to lateral forces applied to the wrist joint or its specialized end portion. Advantageously, the ribs provide for regions of controlled stress and strain when subjected to bending moments, which may be measured by the fiber optic strain gauges 904 embedded in the grooves 917 along the outer surface of the ribs and sensor body parallel to the lengthwise z-axis of tube 906.

In one example, tube 906 and the ribs may be comprised of material with a sufficiently low modulus of elasticity to give a sufficient strain signal under an applied load, a sufficiently high strain at yield to give adequate safety margin above the maximum design load, and a sufficiently high thermal diffusivity to promote rapid thermal equilibrium (therefore reducing thermal disturbances to sensor output signals) when subject to localized or asymmetric thermal disturbances from tissue contact or endoscope illumination. In particular, the plurality of radial ribs may be comprised of a high thermal diffusivity material, such as an aluminum alloy (e.g., 6061-T6 aluminum) or a copper alloy (e.g., GlidCop® AL-60) or a silver alloy to reduce the temperature difference between opposing gauges under transient thermal disturbances by providing a direct thermal pathway between opposing gauges. In yet another example, the plurality of fiber optic gauges 904 may be comprised of a negative thermo-optic coefficient optical fiber material, such as binary or ternary phosphate glass fiber, fluoride glass fiber, oxy-fluoride glass fiber, tellurite glass fiber, or a polymer fiber. The negative thermo-optic coefficient fiber advantageously reduces or eliminates the combined effect of a positive thermo-optic coefficient fiber, such as SMF-28 or other doped fiber, and the positive thermal expansion coefficient of the sensor body material.

In one example, tube 906 may be comprised of metal alloys, treated metals, or plated metals, such as of aluminum, copper, or silver, which allow for adequate strain, mechanical failure safety margin, and high thermal diffusivity. In a further example, 6061-T6 aluminum, which is an aluminum alloy that is heat treated and aged, GlidCop® AL-60, which is copper that is dispersion strengthened with ultrafine particles of aluminum oxide, or a dispersion strengthened silver, may be used to form both tube 906 and the plurality of ribs. Accordingly, both the plurality of ribs and the tube 906 may be comprised of a high thermal diffusivity material, such as an aluminum alloy (e.g., 6061-T6 aluminum) or a copper alloy (e.g., GlidCop® AL-60) or a silver alloy, to reduce transient and/or steady-state temperature differences between groups of strain gauges separated along the z-axis.

Similar to the embodiment described above with respect to FIGS. 6A-6C1, a thermal shielding may be provided over the strain gauges 904 in accordance with another embodiment of the present invention. In one example, a thermal shunt shell 952 is provided over tube 906 with an insulating fluid (gas or liquid) filled or evacuated gap 950 being provided between the outer surface of tube 906 and the inner surface of thermal shunt shell 952. Thermal shunt shell 952 may be mechanically and thermally isolated from the strain gauges by providing compliant elastomer rings 930 between the shunt shell 952 and the tube 906 to prevent interference with the applied surgical forces and to insulate the sensor.

In this embodiment, thermal shunt shell 952 includes an annular heat conducting rib 954 midway between strain gauges 904 in the axial direction (i.e., the z-axis direction). Heat conducting rib 954 contacts an outer surface of tube 906 and conducts heat from the outer shunt shell to the tube 906 such that external thermal disturbances will be more uniformly diffused among the sensors. In one example, heat conducting rib 954 may be comprised of the same material as thermal shunt shell 952, which may be comprised of a high diffusivity material, such as an aluminum alloy (e.g., 6061-T6 aluminum) or a copper alloy (e.g., GlidCop® AL-60) or a silver alloy. Heat conducting rib 954 may be comprised of a different material than thermal shunt shell 952 in other embodiments but will be comprised of a high thermal diffusivity material. Advantageously, the thermal shielding with heat conducting rib midway between the groups of strain gauges as described above allows for more uniform heat/thermal diffusion among the sensors, being particularly advantageous for mitigating asymmetric or transient thermal loads upon the instrument. The thermal shielding described above is applicable for various embodiments of the present invention.

Optionally, a light reflective surface or coating may be provided over thermal shunt shell 952, which may deflect light and reduce localized heating of the force sensor apparatus, for example from endoscope illumination. An insulating coating may also be provided over thermal shunt shell 952, the insulating coating being comprised of a substantially transparent plastic shrink polymer in one example.

Embodiments described above illustrate but do not limit the invention. It should also be understood that numerous modifications and variations are possible in accordance with the principles of the present invention. For example, the number of strain gauges and their configuration may vary but must allow for applicable force and torque determinations and noise rejection. Similarly, the number of ribs and angle between ribs may vary from those described above. Furthermore, the embodiments of force sensor apparatus described above may be integrated with a surgical instrument upon manufacture as a non-separable part of the shaft. Accordingly, the scope of the invention is defined only by the following claims. 

1. A force sensor apparatus, comprising: a tube portion including a plurality of radial ribs and at least one fiber optic strain gauge positioned over each rib of the plurality of radial ribs, wherein the strain gauges are comprised of a negative thermo-optic coefficient optical fiber material; a proximal end of the tube portion operably couplable to a shaft of a surgical instrument that is operably couplable to a manipulator arm of a robotic surgical system; and a distal end of the tube portion proximally couplable to a wrist joint coupled to an end effector.
 2. The apparatus of claim 1, wherein the negative thermo-optic coefficient optical fiber material is selected from the group consisting of a binary or ternary phosphate glass, a fluoride glass, an oxy-fluoride glass, a tellurite glass, and a polymer.
 3. The apparatus of claim 1, wherein the plurality of radial ribs includes one selected from the group consisting of four ribs spaced apart by pairs of supplementary angles about a lengthwise axis of the shaft and three ribs spaced apart by about 120 degrees about a lengthwise axis of the shaft.
 4. The apparatus of claim 1, wherein the plurality of radial ribs includes eight ribs in two groups of four exposed ribs, with each of the ribs in a group being spaced apart by pairs of supplementary angles about a lengthwise axis of the tube portion.
 5. The apparatus of claim 1, wherein the plurality of radial ribs includes six ribs in two groups of three exposed ribs, with each of the ribs in a group being spaced apart by about 120 degrees about a lengthwise axis of the tube portion.
 6. The apparatus of claim 1, further comprising at least one aperture on the tube portion that exposes at least one of the plurality of radial ribs.
 7. A force sensor apparatus, comprising: a tube portion including a plurality of radial ribs and at least one pair of adjacent fiber optic strain gauges positioned over each rib of the plurality of radial ribs; a proximal end of the tube portion operably couplable to a shaft of a surgical instrument that is operably couplable to a manipulator arm of a robotic surgical system; and a distal end of the tube portion proximally couplable to a wrist joint coupled to an end effector.
 8. The apparatus of claim 7, wherein one of the pair of strain gauges over a rib is unstrained and serves as a local thermal correction reference for a strain sensing gauge of the pair of strain gauges.
 9. The apparatus in claim 7, wherein the pair of strain gauges over a rib are in two separate adjacent fibers having different thermo-optic coefficients.
 10. The apparatus of claim 7, wherein the pair of strain gauges over a rib are in two separate adjacent fibers with different core doping.
 11. The apparatus of claim 7, wherein the pair of strain gauges over a rib are in butt fusion spliced pairs having different thermo-optic coefficients.
 12. The apparatus of claim 7, wherein the pair of strain gauges over a rib are in adjacent cores of the same fiber, each core having a different thermo-optic coefficient.
 13. The apparatus of claim 7, wherein the pair of strain gauges over a rib are coincident in orthogonal polarization directions of the same region of a sufficiently bi-refringent stress rod optical fiber.
 14. The apparatus of claim 7, wherein the pair of strain gauges over a rib are coincident in orthogonal polarization directions of the same region of a sufficiently bi-refringent photonic crystal optical fiber.
 15. The apparatus of claim 7, wherein the pair of strain gauges over a rib are coincident in the same fiber core region and have different thermo-optic coefficients by virtue of their different wavelengths.
 16. A force sensor apparatus, comprising: a tube portion including a plurality of radial ribs and a strain gauge positioned over each rib of the plurality of radial ribs; a proximal end of the tube portion operably couplable to a shaft of a surgical instrument that is operably couplable to a manipulator arm of a robotic surgical system; a distal end of the tube portion operably couplable to a wrist joint coupled to an end effector; and a thermal shunt shell over an outer surface of the tube portion.
 17. The apparatus of claim 16, wherein the thermal shunt shell is comprised of a high thermal diffusivity material selected from the group consisting of an aluminum alloy, a copper alloy, and a silver alloy.
 18. The apparatus of claim 16, further comprising one of a fluid-filled gap and an evacuated gap between an inner surface of the thermal shunt shell and an outer surface of the tube portion.
 19. The apparatus of claim 16, further comprising a compliant elastomer ring between an inner surface of the thermal shunt shell and an outer surface of the tube portion.
 20. The apparatus of claim 16, further comprising an annular ring comprised of a high thermal diffusivity material that thermally connects the thermal shunt shell to the tube portion at a point midway between a pair of axially-separated strain gauges.
 21. The apparatus of claim 16, wherein ends of the thermal shunt shell are thermally isolated from the tube portion.
 22. The apparatus of claim 16, further comprising at least one of an insulating material and a light reflective surface or coating over the thermal shunt shell.
 23. A surgical instrument, comprising: a housing portion that interfaces with a manipulator arm of a robotic surgical system; a shaft with a distal tube portion including a plurality of radial ribs along a lengthwise axis of the shaft and a strain gauge positioned over each of the radial ribs, the distal tube portion comprised of a high thermal diffusivity material; a wrist joint operably coupled to the distal tube portion; and an end effector operably coupled to the wrist joint.
 24. The instrument of claim 23, wherein the high thermal diffusivity material is selected from the group consisting of a copper alloy, an aluminum alloy, and a silver alloy.
 25. The instrument of claim 23, wherein the strain gauge is comprised of a negative thermo-optic coefficient optical fiber material.
 26. The instrument of claim 23, wherein the housing portion interfaces with a sterile adaptor that interfaces with the manipulator arm.
 27. The instrument of claim 23, further comprising a thermal shunt shell over an outer surface of the distal tube portion.
 28. The instrument of claim 27, wherein the thermal Shunt shell is comprised of a high thermal diffusivity material selected from the group consisting of an aluminum alloy, a copper alloy, and a silver alloy.
 29. The instrument of claim 27, further comprising one of a fluid-filled gap and an evacuated gap between an inner surface of the thermal shunt shell and an outer surface of the tube portion.
 30. The instrument of claim 27, further comprising a compliant elastomer ring between an inner surface of the thermal shunt shell and an outer surface of the tube portion.
 31. The instrument of claim 27, further comprising an annular ring comprised of a high thermal diffusivity material that thermally connects the thermal shunt shell to the distal tube portion at a point midway between a pair of axially-separated strain gauges.
 32. The instrument of claim 27, wherein ends of the thermal shunt shell are thermally isolated from the tube portion.
 33. The instrument of claim 27, further comprising one of an insulating material and a light reflective surface or coating over the thermal shunt shell. 